基于欧拉角的分导飞行器多模型自适应姿态控制

基于欧拉角的变换得到了刚体飞行器的一种多模型自适应控制律,它能解决转动惯量不确定并随时发生突变的分导飞行器的姿态控制问题.该控制策略可以有效地检测出转动惯量发生突变,并及时切换到最合适的控制器.通过理论分析证明了该控制策略的闭环全局渐近稳定.数值仿真表明该方案的有效性.

Multiple Model Adaptive Control of Post-Boost Vehicles Based on Euler Angles

Based on the transformation of Euler angles, an indirect adaptive control scheme for post-boost vehicles using multiple models and switching is obtained, which can detect the abrupt change of inertia effectively and then switch to the current best controller. Theoretical analysis demonstrates that the overall control system is globally asymptotically stable. A numerical simulation is employed to illustrate the effectiveness of the proposed scheme.